Accession Number : AD0829804
Title : A THREE-AXES ANGULAR ACCELEROMETER TECHNIQUE APPLIED TO VTOL STABILIZATION.
Descriptive Note : Final technical rept., Feb 65-Dec 67,
Corporate Author : TELEDYNE SYSTEMS CO NORTHRIDGE CA
Personal Author(s) : Lease, James E.
Report Date : JAN 1968
Pagination or Media Count : 51
Abstract : This report documents the results of the development, fabrication, and testing of two Angular Reference Systems consisting of two Dual Axis Rate Transducers, one Three-Axis Angular Accelerometer, and the associated electronics required to provide the outputs of angular rate and angular rate summed with angular acceleration about three orthogonal axes. Prototype Angular Accelerometers and electronics were fabricated and integrated with two-axes rate gyros to provide the Angular Reference System for VTOL stabilization. (Author)
Descriptors : (*VERTICAL TAKEOFF AIRCRAFT, STABILITY), (*ACCELEROMETERS, STABILIZATION SYSTEMS), GYRO STABILIZERS, CIRCUITS, DETECTORS, FEEDBACK, ATTITUDE CONTROL SYSTEMS, TRANSDUCERS, COLD WEATHER TESTS, FLIGHT CONTROL SYSTEMS, HYDRAULIC SERVOMECHANISMS, STORAGE, SHOCK(MECHANICS), VIBRATION, MICROELECTRONICS.
Subject Categories : V/STOL
Distribution Statement : APPROVED FOR PUBLIC RELEASE